Modular electronically reconfigurable battery system

ABSTRACT

An electronically reconfigurable battery includes a number of battery modules selectively interconnected by a number of electronic switches, wherein a selectable number of battery modules may be connected either in a series configuration or in a parallel configuration, as a result of placing selected switches of said plurality of switches in open states or closed states. In a parallel configuration, the battery provides power to a primary load, such as a propulsion load for a vehicle. In a series configuration, the battery is configured to provide a high voltage and high power output to a short-term and/or pulsed load, such as an additional load provided on the vehicle. Current from the battery is limited in one of three ways: a) by the batteries themselves; b) a current limiting device or system in series with the total erected battery; or c) a single level power converter or current limiter that is used to erect and charge the capacitor bank in a sequential one level at a time manner until the battery is fully erected and the capacitor is fully charged.

CROSS-REFERENCE TO RELATED APPLICATIONS

This application claims priority to and is a continuation-in-part ofU.S. patent application Ser. No. 10/631,017, filed on Jul. 31, 2003, theentire contents of which are incorporated herein by reference.

BACKGROUND OF THE INVENTION

1. Field of the Invention

The present invention relates to electrical energy storage systems and,in particular, to battery packs composed of multiple battery moduleswith adjustable configurations.

2. Description of the Related Art

Hybrid electric vehicles (HEVs), hybrid electric ships and boats (suchas the QE2) afford greater fuel efficiency than vehicles or vesselshaving only a prime mover (e.g., diesel or gasoline engine, gas turbineand fuel cell). Greater efficiency is obtained by using an energy storeto level the load on the prime mover-providing peaking power to anelectric motor, or storing energy during low power prime mover operationor during regenerative braking.

A well-developed form of energy storage for this application is abattery pack, and there are several candidate battery chemistry systemsthat may be utilized. Of these systems, the lithium-ion (Li-ion)technology is the most energy and power dense. Li-ion cell technologyfor this application is currently capable of energy density of up to 134W-hr (482 kJ) per kg (HE40 cell), and a power density of up to 13 kW perkg (e.g., HP18650 cell short duration, manufactured by SAFT AMERICA).

Vehicle battery packs sized for multiple military combat missions, (suchas the Combat Hybrid Power Systems (CHPS) Systems Integration Lab (SIL)battery pack) store approximately 108 MJ (30 kW-hr). If the highestpower density SAFT cells (HP18650) are utilized, then the short durationpower capability of the battery pack would be greater than 4 MW.

Such a peak power capability could enhance both offensive and defensivecapabilities if it were easily convertible to voltages commensurate witha range of potential short-term and pulsed loads. For example,Electromagnetic Armor (EMA) provides lightweight protection to combatvehicles against rocket-propelled grenade attacks. The energy requiredfor the EMA to function is stored in a fast discharge capacitor bank,which is recharged either from a generator operated by the prime moverof the vehicle, or from an intermediate energy storage system. In a HEV,the electric energy battery pack also could function as such anintermediate energy storage system. However, in order to provide theapproximately 10 kV needed as the input voltage to the capacitor bank, aDC-DC power converter is needed between the intermediate energy storagesystem and the capacitor bank.

The traditional methods for DC-DC power conversion typically involve theuse of inverters and heavy-duty transformers. Current EMA designsrequire approximately 150 kJ to recharge the capacitor bank. At 3 pulsesper second (pps) operation, even for a short period of time, therecharge time would have to be on the order of 300 ms. Consequently, therecharge power would have to be on the order of 500 kW average, or 1 MWpeak. However, a 1 MW peak power traditional DC-DC converter, usingpresent technology, would add more volume and mass to the vehicleplatform than is allowable in a 16-20 ton class vehicle.

Thus, there exists a need in the art for a system power densityimprovement in producing short term high power at high voltages from abattery pack normally configured to provide hybrid vehicle prime moverload leveling and/or silent mobility capability or in other fixed ormoving battery platforms such as battery backpack systems or pulsedenergy weapons or launch systems.

SUMMARY OF THE INVENTION

The present invention provides an alternative method for converting DCfrom bus voltage to a voltage that is compatible with various loads.According to the present invention, a battery pack is electronicallyre-configured to produce multiples of a bus voltage, momentarily and oncommand. Such a battery pack would be configured in modules that areequal to the power distribution bus voltage. The entire battery pack, orsome fraction thereof, can be erected and de-erected on command,analogous to the operation of a Marx generator (commonly used forcapacitive voltage multiplication).

According to embodiments of the present invention, the need forintermediate DC-DC power conversion circuitry is reduced or eliminatedby using electronic switching to convert the battery pack modules fromtheir normal parallel configuration for vehicle or ship load levelingand/or silent mobility functions, to a series configuration that iscapable of delivering the necessary high power and high voltage outputfor short-term and pulsed load operations.

In particular, according to a first preferred embodiment, the presentinvention provides an electronically reconfigurable battery, including afirst number of battery modules, a number of switches selectivelyinterconnecting the battery modules, wherein a selectable number of thebattery modules may be connected either in a series configuration or ina parallel configuration, as a result of placing selected switches ofthe switches in open states or closed states, and an output switchconnecting a first output terminal of the battery to a first load. DCcurrent flow is limited and controlled by electrochemical DC currentdischarge characteristics of the battery technology used, such as in thecase of lithium-ion (Li-ion) technology.

In another embodiment of the present invention, an electronicallyreconfigurable battery includes a first number of battery modules, anumber of switches selectively interconnecting the battery modules, anda current limiting section or a current limiting DC-DC converter,wherein a selectable number of the battery modules may be connectedeither in a series configuration or in a parallel configuration, as aresult of placing selected ones of the switches in open states or inclosed states, and an output switch connecting a first output terminalof the battery to a first load.

The DC current limiting device can be used to control the currentoutside the range of the electrochemical DC current dischargecharacteristics of the battery technology used. A parallel operation DCby-pass switch is optionally incorporated within the current limitingsection dependent on the technology used and where the section islocated at the beginning or end of the series connected batteries. Asimple example of this current limiting section is a series connectedpower resistor, or inductor connected in series between the high voltagebattery end terminal and a Pulse Forming Network capacitor bank(commonly known as a PFN capacitor) forming the resistive, the inductiveor resonant capacitor charging circuit.

According to another embodiment of the present invention, anelectronically reconfigurable battery includes a first number of batterymodules, a number of switches selectively interconnecting the batterymodules, a single stage current limiting section or a single stagecurrent limiting DC-DC converter (hereinafter referred to as a singlestage converter or SSC). The SSC may take the form of a resistor orinductor or a reduced size electronic DC-DC converter using some form ofBuck, Boost, Buck/Boost or Resonate or inductive converter topology,wherein a selectable number of the battery modules may be connectedeither in a sequential series configuration operation or in a parallelconfiguration, as a result of placing selected switches of the switchesin open states or closed states, and an output switch connecting a firstoutput terminal of the battery to a first load.

A DC current limiting device can be used to control the current outsidethe range of the electrochemical DC current discharge characteristics ofthe battery technology used. A parallel operation DC by-pass switch isoptionally incorporated within the current limiting section dependent onthe technology used and whether the section is located at the beginning,end or middle of the series connected batteries.

According to another embodiment of the present invention, the system maybe configured to be redundant and fault tolerant in most applicationsand is capable of bidirectional power flow. Additionally, the system canbe built in either a discrete or stackable modular form. The system mayinclude one or more voltage scalable arms that are configured in a“star” or “H” configuration with switch steering matrixes both in theinner and outer portions of the star configurations. These switchingarrays can also be used to cross-connect multiple star configurationsand isolate the loads from the ERB sections. The multiple arms may beconnected at one end for the parallel Low voltage or Baseline Voltageoperation using inner (base) switch matrix or direct hardwired connectedbetween the multiple arms. The other end of each arm is connected to theSeries or variable high voltage (VHV) connection. The energy from thebase side connection of each arm is fed in parallel to the center switchmatrix primarily to provide traction power or the main system load. Thisvoltage is normally fixed at the module's base voltage level. The Energystored in the arm can also be directed to flow out the opposite end ofthe each arm through the VHV connection into an outer switch matrix ormultiple outer switch matrixes at different voltage levels that connectsto auxiliary loads or pulse power loads. The Energy flow is in discreteenergy packets that are time multiplexed on the VHV connection sidewhile maintaining a continuous connection and energy flow through thebase or parallel connection side. The modules can be erected andde-erected at high speed in series and parallel combinations allowingthe VHV output to be continuous, or rising stair case step voltage or apulsed voltage and energy output. Thus, the VHV output connection isallowed to charge and transfer energy from the base voltage energystorage system through the VHV steering matrices to much higher voltageenergy storage systems located at or near the auxiliary high voltageloads.

Each arm may be composed of a group of smart reconfigurable identicalenergy modules that each contain, in the least: a base power source,such as 720 Volt battery stack; a stackable intermediate pass-throughswitch matrix; an inter-module interconnect bus bar system; protectionsystems; and a distributed control system. The modules in each arm canbe electronically reconfigured themselves to connect in parallel to theparallel inner bus structure at the base voltage or to be disconnectedfrom the parallel inner bus structure. Additionally, the modules can beconfigured to transfer and redirect energy out of the VHV connectioninto the multiple output switch or output steering matrixes to theauxiliary HV energy stores by and raising the voltage and pulsing theenergy out of the VHV connection.

The energy packets can be controlled in two dimensions: discrete voltagesteps and time. The variable voltage has discrete voltage steps that arethe same voltage level as the individual module stages; the number ofsteps is determined by the number of modules. The VHV voltage can beraised to the value of the base voltage multiplied by the number ofmodules in the arm connected in series. Each module can have two highpower input and two high power output connections, a digitalcommunication port or ports, and an auxiliary power input.

Notably, this system is substantially different from otherreconfigurable battery or energy sources in that the series parallelswitch matrix and bus bars are an integral part of the module and it canfunction as a “plug and play” system with modules in parallel mode ofoperation with two arms in parallel as clearly detailed in FIG. 8. Thatis, any of the modular diagrams FIGS. 1-6 can be used in FIG. 7 or 8configurations. FIGS. 1-6 also show only the positive output version ofthe arm connections. For negative output arm connection simply the inputand output connection are reversed as shown in detail H configurationFIG. 8 and move the current limiting or active conditioning systems asshown in FIGS. 2-5 to the opposite end.

For positive output, the base or the parallel input shown in FIGS. 7-8are the same input or low voltage parallel connection as static storeconnections (207) of FIG. 2. Vehicle mobility battery and loads as shownin FIG. 3. Static store (442) in FIG. 4. the static store connection ofFIGS. 5 and 6

Each of the single arm configurations shown in FIGS. 1-6 have a singlediode HV matrix switch, labeled D1 built into the end module the diodelocated in the last module and at the end of the High voltage chain orarm. The connection at cathode end of the diode is the normal HV output.In FIG. 8-9, and the diode matrix is external to the modules, resultingin identical modules.

Thus, the maximum voltage can be changed by adding or subtracting plugin module without any bus bar or switch matrix changes. For example, afour arm “star” configuration—the “H” configuration—has one end of eacharm connected in parallel at the center of the star connected to the 720volt traction drive system and four outer ends of the arms creating two+5.7 Kilovolt variable voltage sources and two −5.7 Kilovolt sources.The outer steering switch matrix in this case can include 4 high voltagediodes and two pairs of arms are essential in parallel for redundancyfor continued operation after sustaining faults or battle damage. The11.4 kV (kilovolt) differential voltages are used to charge a 150 kJpulsed power 10 kV capacitor bank. Each arm consists of 8 modules whichtranslates to 32 (i.e. 8×2×2) modules in parallel operation. When usedin a high performance traction drive, the energy packets can be timemultiplexed between the drive system and erecting the 11.4 Kv pulsedpower system. Total elapsed time for charging the capacitor bank isunder 500 milliseconds.

In a more complex embodiment, with additional arms and sophisticatedoutput load switch matrix added, energy packets can deliver energy toloads between 720 and 5.7 kV. Using the same modules, the system isscaled up to a 30 kV pulsed power application by simply adding moremodules in series.

There are several differences between this system and otherreconfigurable battery systems that have been around since the firstbattery powered trucks and cars. First, this system is designed for atleast two output or loads that have different voltage requirements.Second, this topology is based on a “Star or H” Configuration withmultiple reconfigurable energy storage and production arms with multipletime multiplexed outputs. Finally, there is an inner and outer switchmatrix for controlling and directing the voltage and energy anintermediate switch matrix that is distributed among the modules eachmodule contains the battery pack or energy source, the switch gear andbus work.

This more complex reconfigurable electrical energy storage system isespecially useful in hybrid electric vehicles, ships, or boats (i.e.,vehicles, ships, or boats powered by both a prime mover and anelectrical energy power source) used in military operations and in otherfixed or moving platforms where it is desirable to be able to redirectand level shift the stored energy in the reconfigurable electricalenergy storage system to auxiliary higher voltage energy storage anddeliver systems such as pulsed power weapon and protection systems.Examples of such reconfigurations include a shift from a low voltageparallel configuration to high voltage series/parallel configurationsfor optimizing impedance match, minimizing or eliminating the need foran associated power converter for pulsed power applications, poweringother subsystems or matching variable DC link main systems as envisionedin, for instance, the original CHPS combat hybrid vehicle, which shiftedfrom a 300-400V low voltage parade voltage to a higher 900-1200V combatstatus bus voltage.

Another embodiment of the present invention employs a modular scalableelectric power distribution topology having multiple outputs to transferenergy and power between loads and sources of different operatingvoltages simultaneously. This transfer can occur in either a continuousor time multiplexed manner consisting of one or more reconfigurableenergy storage or production ERB arms connected in the ““star or H””configuration. Each of the two ends of an ERB arm has a bidirectionalpower output connection referred to as the base or parallel outputconnection and the high variable high voltage (VHV) output connection.

Three switch or steering matrix arrays can be used for directing andcontrolling the energy flow. The first array includes an inner or baseswitching array located at the center of the star configuration forparallel combinations of the parallel or base voltage. The second arrayincludes an intermediate switching matrix array distributed along eacharm in the modular sections for parallel and series module combinations.The third array includes an output matrix or steering array or arrays todirect the VHV output from each ERB arm. The VHV array connects themultiple arms of the VHV outputs to the various multiple auxiliarystorage systems or loads at voltages higher than the center basevoltage.

Each energy storage or production ERB arm consists of a building blockmodular system in discrete or modular form consisting of multipleidentical interface modules. The ERB modules contain an energy storagedevice such as a battery or capacitor or an energy production ortransformation module such as a fuel cell or a power conversion devicesuch as a solid state converter as shown in the text body. Additionally,each ERB module contains a piece of the distributed modular intermediatebus structure and switch matrix steering array as well as a part of thedistributed control system and algorithms to prevent faults,misconnections and catastrophic failures due to mistiming of switchelements.

Another embodiment of the present invention may employ a method oftransferring energy from one voltage and intermediate energy storage orenergy production system to a higher or lower voltage energy storagesystem or load.

Another embodiment employs a simple switching algorithm and a threeswitch and one diode configuration that guarantees no catastrophicbattery or fire failures due to mistiming of the in high speed switchingor modulating of the series connection switches in the intermediatedswitch array. This is accomplished by switching off or opening all ofthe positive and negative rail switches rail switches labeled P and N insimplified parallel operation diagram, then using just the one seriesswitch connection labeled S and one Required steering diodes per moduleallows seamless high speed erecting and de-erecting of the batteries orcapacitors in series or series voltage stepped VHV Output by selectingthe number of series switches turned on or sequenced with no criticaltiming issues.

In another embodiment the base switch matrix can be effectively set to‘ON’ at all times by replacing the switch matrix with hard wiredparallel connections of the base voltage terminals of the ERB Arms. Onenotable improvement of this invention over the prior art is that itallows simple scaling of more by the simple addition of more moduleswithout any rewiring due to its modular and scalar design. SophisticatedERB systems with complete redundancy of the ERB star and multiple starconfigurations are easily configured by switched in and cross connectedat the base and/or at the VHV level matrix levels.

In an alternative embodiment, VHV outputs can be steered in paralleloperation through a simple VHV diode steering array. This allowscomplete or partial failure of one more ERB arms without rendering thesystem inoperative. Two sets of two arms each supply energy in parallelto the 10 Kv 150 kJ energy storage capacitor. As a result, the systemcan suffer a complete failure of one plus and one minus output ERB armand still meet VHV mission requirements. Furthermore, the system cansuffer the loss of three ERB arms before losing traction or movingcapability. A multiple arms configuration, such as the “star” or “H”, isa great improvement over the single arm ERB configuration becauseparallel operation battery source resistance or ESR (Equivalent seriesresistance) is reduced by a factor of 4, or the number of arms inparallel.

In an alternative embodiment the ERB module can be “plug and play”. Inthis form, the module consists of a stand alone self contained modulewith simple power two input port connections and two output powerconnections. The energy source, part of the modular distributed seriesand parallel switch matrix and bus bar system, fusing and protection andcontrol system are all internal to the module. The Power ports can bedirectly connected to another module. In each ERB arm, first designatedmodule input ports are connected to the base or parallel operation busor matrix. The output of the first module is connected to the input ofthe second module in the module string in the ERB arm continuing in thisfashion until the last module in the string is connected and the outputport connection now become the VHV connection to the VHV steering array.Very high voltages can be achieved in this fashion, and 30-40 kv systemscan be designed using this building block approach. Because of itsscalability, the number of modules per ERB arm is application drivenand, in a multiple arm ERM “star” configuration system, each arm mayhave a different number of modules and have a different polarization anoutput voltage to satisfy a wide variety of load requirements.

In another embodiment nested ERB are used. Nested, or layered, ERB areERB systems with nested or layered ERB are contained within each levelof stackable modules. The next level of ERB is to use an ERB within theERB module to reduce the base voltage and basic module voltage. Anexample is reducing a 720 volts ERB module to a lower voltage 36 voltsERB module using ten (10) sub ERB modules within each 720 volt ERBmodule. The advantage is it allows the Base voltage to be dropped andallows a finer resolution in the high voltage output example 10 submodules×8 modules=80 voltage steps resolution in the VHV output. Thisallows the Base current in parallel operation to be ten times higher forhigh torque low speed application or to create long life parade groundlow voltage power and shorter life high speed combat modes.

The reconfigurable electrical energy storage system may combine one orall one or all of the above-mentioned features.

Further applications and advantages of various embodiments of thepresent invention are discussed below with reference to the drawingFigs.

BRIEF DESCRIPTION OF THE DRAWINGS

FIG. 1 is a block diagram of a hybrid electric vehicle platform powerdistribution system including an electronically reconfigurable batteryaccording to an embodiment of the present invention;

FIG. 2 is a schematic diagram of an electronically reconfigurablebattery according to an embodiment of the present invention, adapted foruse with an electromagnetic armor (EMA) system for a combat hybridelectric vehicle and other platforms;

FIG. 3 is a schematic diagram of an electronically reconfigurablebattery according to an embodiment of the present invention, adapted toa generic use;

FIG. 4 is a schematic diagram of an electronically reconfigurablebattery including a current limiting section according to an embodimentof the present invention, adapted for use with an electromagnetic armor(EMA) system for a combat hybrid electric vehicle and other platforms;

FIG. 5 is a schematic diagram of an electronically reconfigurablebattery including a single stage converter (SSC) according to anembodiment of the present invention, adapted for use with anelectromagnetic armor (EMA), ETC Gun, pulsed laser, pulsed beam, energyor particle source systems for a combat hybrid electric vehicle andother platforms;

FIG. 6 is a schematic diagram of an electronically reconfigurablebattery including a single stage buck/boost converter section (SSC)according to an embodiment of the present invention, for use with anelectromagnetic armor (EMA), ETC Gun, pulsed laser, pulsed beam, energyor particle source systems for a combat hybrid electric vehicle andother platforms.

FIG. 7 is a schematic diagram of a simplified “H” or “star”configuration ERB system according to an embodiment of the presentinvention.

FIG. 8 is an illustration of an “H” configuration ERB system accordingto an embodiment of the present invention.

FIG. 9 is a schematic view of a scalable ERB arm for use in an “H” or“star” configuration ERB system according to an embodiment of thepresent invention.

DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS

The term “star” configuration refers to novel battery configurationshaving 2 or more battery arms, which will be understood from thedescription below and the drawing figures. The “H” configuration refersto a “star” configuration with only 4 arms and is a subset of starconfigurations. Star configurations are not limited in the number ofarms they can have.

Dependent on the system configuration, common modules can be configuredinto multiple arms with positive or negative high voltage output withHigh Voltage Steering diode or HV Steering diode switch matrixes andwith one or multiple inner starring and disconnect switch matrixessurrounding common hub parallel connection.

For simplicity sake, FIGS. 7-8 show a star configuration with 4 arms orchains of strings of modules depicted in FIGS. 1-6. However, the numberof arms in these exemplary star configurations could have been 8, 9 or10 arms or higher. In fact, it is contemplated that the presentinvention could be implemented with 1000 or more arms.

As shown in FIG. 1, a hybrid vehicle platform power distribution system100 includes a prime mover 101 (e.g., diesel engine, gas turbine, fuelcell, etc.) coupled to the vehicle transmission (gears) 102, and ann-phase electric motor 103 coupled directly to the drive wheels of thevehicle 109. The gears also are coupled to a generator 104 forrecharging the electrical energy storage (ERB energy store) 105, forexample, during regenerative vehicle braking and during low power primemover operation. The ERB energy store 105 functions to power the n-phasemotor 103 for vehicle load leveling and/or silent mobility operation,and also is used to provide power to various short-term and pulsed loaddevices 106. Power electronic circuitry 107 controls the reconfigurationof the ERB, the interfacing between the generator 104, motor 103, ERBstore 105, and short-term and pulsed loads 106, as well as providingappropriate bus voltage to a voltage bus (hotel bus) 108.

As shown in FIG. 2, an electronically reconfigurable battery 200according to the first embodiment of the invention includes a number ofbattery modules 201. An example of such a battery module is anUltralife® lithium polymer rechargeable battery module (e.g., UBC44 orUBC38). Other candidate modules include, but are not limited to, SAFT HPcells (such as HP 12, HP 6, and HP 18650).

The battery 210 includes a number of modules that are permanentlyconfigured in parallel with each other (static store) 207 and connectedto the vehicle load bus 211, which powers the electric motor. Othermodules (dynamic store) 208 can be switched between parallelconfiguration to support the vehicle load bus 211, and a seriesconfiguration to charge the EMA capacitor bank 209 (or other short-termor pulsed load not shown). The electronic reconfiguration of the dynamicstore modules 208 requires three switches per module.

An erectable battery module 201 is associated with battery isolationswitches 202 and 203, and a series switch 204. All switches (with theexception of the output switch 205) need only block the voltage of asingle battery module and open at near zero current (for capacitorcharging) in normal operation. Transient conditions during erection andde-erection are controlled by passive snubbing. Reconfiguration can beaccomplished in less than 1 ms using standard off-the-shelf solid stateswitches such as integrated gate bipolar transistors (IGBT) or MetalOxide Field Effect Transistors (MOSFET).

Switches 202, 203, and 204 can be rated for the module voltage (such as1 kV) only. Switch 205 is an output switch that is rated for the fulloutput of the ERB (e.g., 10 kV and 100 amps), and can be implemented asa series stack of the same switches used for switches 202, 203, and 204.A vacuum contactor 212 and fuse 213 are placed in series with the outputswitch 205 to provide fault protection and charge interrupt. Allswitches are preferably opto-isolated, with gate power drawn from theirassociated adjacent battery modules. Switch 206 is high-voltagehigh-current closing switch, and can be either a vacuum switch or asolid state switch. Switch 206 discharges the EMA capacitor bank intothe EMA load.

With some 8,000 cells necessary to make up a 30 kW-hr vehicle batterypack, voltages would be available in multiples of the distribution busvoltage up to 30 kV. Furthermore, each of these voltage levels isavailable with the full power capability of the battery pack.Construction techniques used in the HP18650 are scaleable to larger orsmaller individual cells so that optimization for the particularapplication is possible.

Example

Assuming a 20-ton class vehicle and extrapolating from CHPSrequirements, a conceptual design of an ERB for a hybrid electricvehicle with an EMA system has the following requirements: 1) Deliver upto 400 kW to the vehicle bus at 1 kV in parallel operation; 2) Rechargea 150-kJ capacitive store to 10 kV in 300 milliseconds; and 3) Support30-45 minute silent operation at 80 kW. These requirements mandate theuse of very high energy and power density batteries. Two candidatebatteries are the HP series of lithium ion batteries being developed bySAFT and the lithium polymer batteries produced by Ultralife Batteries,Inc. for use in cell phones. The SAFT batteries have a slight advantagein usable power density and packaging for military use, whereas theUltralife batteries have an advantage in cost (0.15-0.2 cents/J, 5-8cents/Wpk, owing to volume production) and a potential for more compactpackaging (prismatic) in ERB service.

The ERB system in this case constitutes only ⅓ of the total battery forerected (dynamic) operation. The remaining ⅔ of the store (static) isdedicated to load leveling and silent mobility. The total capacity of˜290 MJ (80 kW-hr) accommodates silent mobility requirements. With only⅓ (90 MJ, 25 kW-hr) of the total capacity configured for on-commandelectronic erection and de-erection, the vehicle energy storage systemmaintains its load leveling and silent operation capability even whenthe EMA is active.

54 series×7 parallel Ultralife Model UBC44106102 polymer batteries areassembled into 200-volt stacks (378 cells per pack), in the staticstore. Five of these packs are placed in series to obtain an outputvoltage equal to that of the vehicle bus and constitute a module. Twosuch modules in parallel make up the static store (3780 cells total). Inthe dynamic portion of the store, the UBC383562 cell is used because ofits heavier tabbing and proven current capability. The 200-volt packs inthis case consist of 54 series×4 parallel cells (216 total). Five suchpacks make up an erectable module and there are 10 modules, thusproviding 10 kV on command for EMA store charging (approximately 90 MJ;10,800 total cells). A dynamic module will incorporate all necessaryswitches, isolation and thermal management hardware. The total batteryvolume in the static store is approximately 0.18 m3 and the accessoriesare expected to add another 0.135 m3 for a total volume of approximately0.315 m3 and a mass of 620 kg. The dynamic store is less efficientvolumetrically, because for the need to insulate for the 10 kV momentaryoperation and thermal stress associated with MW-class power for even afew seconds. We expect a battery volume of 0.089 m3 with a total ofvolume of 0.314 m3 and a mass of 500 kg, when accessories are included,for the dynamic store. These total to a volume of 0.629 m3 and mass of1120 kg for the entire vehicle battery pack (˜300 MJ).

FIG. 3 shows a generic application of the ERB system 300 according to anembodiment of the invention, wherein the ERB charges an energy storerepresented by a capacitor 330, which is discharged via a switch 332into a load represented by a resistor 334.

FIG. 4 shows another embodiment 400, which has the same configuration asFIG. 2, with the PFN 440 represented by a block, and further including acurrent limiting device 441 inserted between the static 442 and dynamic443 portions of the battery.

FIG. 5 shows another embodiment 500, which has the same configuration asFIG. 4 except with a SSC 550 replacing the current limiting device, anddiodes 551, 552 and 553 added as steering diodes. The charge sequence isdifferent from the first and second embodiments, in that a sequentialstep charge mode of operation can be used with the circuit of FIG. 5,also the list of applicable loads is expanded and can be applied to allembodiments.

FIG. 6 is an alternate example of another embodiment of the presentinvention. The ERB 600 is configured for a sequential step charge modeusing a Buck/boost PWM single stage converter (SSC) type. The high-speedsemiconductor switches U1, U2 can be bipolar transistors, MOSFETs,IGBTS, SCR and other power semiconductor switches. Other converter typessuch as buck, boost and other electronic converter topologies aresimilar in operation and also can be used for the switching regulator.

Example of Sequential Step Charge Operation

The sequential step charging operation mode using a single stageconverter (SSC) as shown in FIGS. 5 and 6 is described below.

The best location for the single stage converter 650 is between thestatic 660 and dynamic 670 portion of the battery as this limits thevoltage stresses seen by the internal components, but the SSC 650 can belocated anywhere within the series-connected loop that starts with thestatic store 660 portion of the battery and ends with the PFN capacitorbank 680. A single inductor 651, non-isolated buck/boost or interleavedbuck/boost configuration is the preferred topology. A by-pass switch S29will normally be employed in this location to connect the dynamicportion 670 of the battery to the static portion 660 in a low lossmanner, bypassing the SSC 650 in the parallel mode of operation.

In the series sequential charge operation, the PFN capacitor bank 680 ischarged in ten (10) sequential steps.

First, the switches of the dynamic store portion 670 of the battery areall opened except for the positive isolation set of switches; the SSC650 is now directly connected between the static portion 660 of thebattery and the PFN capacitor 680.

Next the SSC 650 is turned “ON” and charges the PFN capacitor bank 680at a controlled current (100 A) to approximately slightly more(1010-1200V) than the single battery module voltage (1000V) at whichpoint it shuts down momentarily and a battery module is erected inseries with the SSC 650 by selectively opening and closing theappropriate switches. The SSC 650 is turned back “ON” and PFN capacitorbank 680 charges at the controlled current until the SSC 650 reaches itscontrolled output voltage set point at which time it will shut offagain.

The stored voltage in the PFN capacitor bank 680 is now V (SSC)+batteryV1 (2010-2200V).

The cycle is repeated until all the batteries with the SSC 650 areerected in series, or the desired stored PFN voltage set point isreached (V PFN=(V (SSC)+batteriesV1+V2+V3+V4+V5+V6+V7+V8+V9=(900-10200V)). By using this method the powerprocessing capability required of the SSC 650 is reduced from the systemlevel power delivered (10 kV @100 A) by the number of battery stageserected plus one (in this case 10) for a (SSC) nominal power rating of1000 v @100 A or 100 kW. This reduces the converter size by a factor ofmore than ten because the converter has 1/10 of the voltage stresses andno longer needs an isolation or step-up transformer. PFN voltageregulation is finer and smoother than the first embodiment; however thefirst embodiment is the smallest physically, the most robust and is thecheapest to build.

Normal Operation

As shown in FIGS. 5 and 6, the dynamic part of the battery store isconnected as nine parallel 1000 volt batteries (V1-V9) connected inparallel with the main or static portion (V10-V11) of the batterysystem. In normal operation, negative isolation switches S3, S6, S9,S12, S15, S18, S21, S24, S27 and positive isolation switches S2, S5, S8,S11, S14, S17, S20, S23 and S26 are closed, and bypass switch S29 in theSSC is closed. Battery series switches S4, S7, S10, S13, S16, S19, S22,S25 and S28 as well as HV contactor S1 are open. The battery now has 11parallel sections to power a vehicle.

ERB Dynamic Operation

The ERB dynamic section 670 is erected in 10 steps, which are nowexplained with reference to FIG. 6.

Step one—Converting from Static to Dynamic mode and Single Stageconverter (SSC) charging of the Pulse Forming Network (PFN) from 0 to1200 volts

The shift from static to dynamic operation begins with the SSC 650bypass switch S29 and all negative isolation and series connectedswitches being opened. All positive isolation switches are kept closedand HV contactor S1 switches from being opened to closed.

The SSC 650 then switches to a charge mode and begins charging the PFNstorage capacitor bank 680 at an average current of 100 Amperes. Thecurrent flow path is through positive switches S2, S5, S8, S11, S14,S17, S20, S23 and S26, which then forward bias diode D1, allowing thecurrent to flow through HV contactor S1 into the PFN capacitor bank 680.At a PFN charge voltage of 1200 volts, the SSC 650 stops charging andgoes into an idle mode for the Step 2 ERB configuration change. Currentflowing into PFN stops and goes to zero.

SSC Charge and Idle Modes of Operation

In the charge mode of operation, for SSC 650 Voltage Output (Vout) rangefrom zero to approximately 1000 volts, the SSC is in a step—down buckregulator mode with solid state high speed semiconductor switch U2 openand solid state high speed semiconductor switch U1 operating in avariable duty cycle Pulse Width Modulation (PWM) scheme to maintain anaverage output current of 100 A (I out). For the Vout range from1000-1200 volts, the SSC 650 shifts to a step-up boost mode and U1 isnow on at a 100% duty cycle, and U2 is PWM modulated to control theoutput current.

When Vout reaches 1200 volts, the SSC 650 is put in idle mode and U2 isthen turned on at 100% PWM and the SSC voltage output and current dropto zero. The loss of the SSC Vout of 1200 volts results in reversebiasing diode D1 as the voltage difference between the PFN voltage andthe dynamic store section is −1200 volts. The current flow through thedynamic store battery section 670 falls to zero due to the reversebiasing of Diode D1. Average current in the SSC's inductor is maintainedby PWM modulating U1 while U2 is 100% on. At this point the processproceeds to step two.

Step two—Erecting first battery stage—PFN charging voltage of 1200-2200volts

SSC starts the step 2 cycle in IDLE mode, Vout and Iout are at zero,negative switches S3, S6, S9, S12, S15, S18, S21, S24, and S27 are open.Switch S2 now opens and switch S4 now closes, connecting battery V1 inseries with the SSC output. The SSC 650 now switches back to CHARGE modeand charges the PFN from 1200 volts to 2200 volts by the series voltageaddition of SSC Vout and V1 (1000V). Again Vout only varies over a rangefrom 0-1200 Volts. At PFN charge voltage of 2200 volts, the SSC 650 goesback into IDLE mode for the Step 3 ERB configuration change.

The amount of time needed for the SSC 650 to be in the IDLE mode isdetermined by the time required for the diode D1 current to fall to zeroand the time required to set the ERB switches to the new configuration.Total IDLE time per step change is estimated to be in the 10-100microsecond range.

Step 3—Erecting second battery stage—PFN voltage 2200-3200 volts:

SSC starts step 3 cycle in IDLE mode, Vout and Iout are at zero,negative switches S3, S6, S9, S12, S15, S18, S21, S24, and S27 are open.Switch S2 is open and switch S4 is closed. Switch S5 is now opened andswitch S7 is now closed, connecting batteries V1 and V2 in series withthe SSC output. The SSC 650 now switches back to CHARGE mode and chargesthe PFN from 2200 to 3200 volts by the series voltage addition of SSCVout and V1, V2 (2 kV). Again, Vout only varies over a range from 0-1200volts. At PFN charge voltage of 3200 volts, the SSC goes back into IDLEmode for the Step 4 ERB configuration change.

Step 4—Erecting Third battery stage—PFN voltage 3200-4200 volts:

The SSC starts step 4 cycle in the IDLE mode, Vout and Iout are at zero,negative switches S3, S6, S9, S12, S15, S18, S21, S24, S27 are open.Switches S2, S5 are open and switches S4, S7 are closed. Switch S8 isnow opened and switch S10 is now closed, connecting batteries V1, V2,and V3 in series with the SSC output.

The SSC 650 now switches back to CHARGE mode and charges the PFN from3200 to 4200 volts by the series voltage addition of SSC Vout and V1,V2, V3 (3 kV). Vout varies over a range from 0-1200 volts. At PFN Chargevoltage of 4.2 kV, the SSC goes back into IDLE mode for the Step 5 ERBconfiguration change.

Step 5—Erecting Fourth battery stage—PFN voltage 4200-5200 volts:

SSC starts step 5 cycle in IDLE mode, Vout and Iout are at zero,negative switches S3, S6, S9, S12, S15, S18, S21, S24, S27 are open.Switches S2, S5, S8 are open and switches S4, S7, S10 are closed. Switch14 is now opened and switch 16 is now closed, connecting batteries V1,V2, V3, and V4 in series with the SSC output.

The SSC 650 now switches back to CHARGE mode and charges the PFN from4200 to 5200 volts by the series voltage addition of SSC Vout and V1,V2, V3, V4 (4 kV). Vout varies over a range from 0-1200 volts. At PFNCharge voltage of 5200 Volts, the SSC goes back into IDLE mode for theStep 6 ERB configuration change.

Step 6—Erecting Fifth battery stage—PFN voltage 5200-6200 volts:

SSC 650 starts step 6 cycle in IDLE mode, Vout and Iout are at zero,negative switches S3, S6, S9, S12, S15, S18, S21, S24, S27 are open.Switches S2, S5, S8, and S11 are open and switches S4, S7, S10, and S13are closed. Switch 14 is now opened and switch 16 is now closed,connecting batteries V1, V2, V3, V4, and V5 in series with the SSCoutput.

The SSC 650 now switches back to CHARGE mode and charges the PFN from5200 to 6200 volts by the series voltage addition of SSC Vout and V1,V2, V3, V4, V5 (5 kV).

Vout varies over a range from 0-1200 volts. At PFN Charge voltage of6200 Volts, the SSC goes back into IDLE mode for the Step 7 ERBconfiguration change.

Step 7—Erecting Sixth battery stage PFN voltage 6200-7200 volts:

SSC 650 starts step 7 cycle in IDLE mode, Vout and Iout are at zero,negative switches S3, S6, S9, S12, S15, S18, S21, S24, S27 are open.Switches S2, S5, S8, S11 and S14 are open and switches S4, S7, S10, S13and S16 are closed. Switch 17 is now opened and switch 19 is now closed,connecting batteries V1, V2, V3, V4, V5 and V6 in series with the SSCoutput.

The SSC 650 now switches back to CHARGE mode and charges the PFN from6200 to 7200 volts by the series voltage addition of SSC Vout and V1,V2, V3, V4, V5, V6 (6 kV).

Vout varies over a range from 0-1200 volts. At PFN Charge voltage of7200 Volts, the SSC goes back into IDLE mode for the Step 8 ERBconfiguration change.

Step 8—Erecting Seventh battery stage PFN voltage 7200-8200 volts:

SSC 650 starts step 8 cycle in IDLE mode, Vout and Iout are at zero,negative switches S3, S6, S9, S12, S15, S18, S21, S24, S27 are open.Switches S2, S5, S8, S11, S14 and S17 are open and switches S4, S7, S10,S13, S16 and S19 are closed. Switch 20 is now opened and switch 22 isnow closed, connecting batteries V1, V2, V3, V4, V5, V6 and V7 in serieswith the SSC output.

The SSC 650 now switches back to CHARGE mode and charges the PFN from7200 to 8200 volts by the series voltage addition of SSC Vout and V1,V2, V3, V4, V5, V6, V7 (7 kV).

Vout varies over a range from 0-1200 volts. At PFN Charge voltage of8200 Volts, the SSC goes back into IDLE mode for the Step 9 ERBconfiguration change.

Step 9—Erecting Eighth battery stage PFN voltage 8200-9200 volts:

SSC 650 starts step 9 cycle in IDLE mode, Vout and Iout are at zero,negative switches S3, S6, S9, S12, S15, S18, S21, S24, S27 are open.Switches S2, S5, S8, S11, S14, S17 and S20 are open and switches S4, S7,S10, S13, S16, S19 and S22 are closed. Switch 23 is now opened andswitch 24 is now closed, connecting batteries V1, V2, V3, V4, V5, V6, V7and V8 in series with the SSC output.

The SSC 650 now switches back to CHARGE mode and charges the PFN from8200 to 9200 volts by the series voltage addition of SSC Vout and V1,V2, V3, V4, V5, V6, V7, V8 (8 kV).

Vout varies over a range from 0-1200 volts. At PFN Charge voltage of9200 Volts, the SSC goes back into IDLE mode for the Step 10 ERBconfiguration change.

Step 10—Erecting Ninth battery stage PFN voltage 9200-10200 volts:

SSC 650 starts step 10 cycle in IDLE mode, Vout and Iout are at zero,negative switches S3, S6, S9, S12, S15, S18, S21, S24, S27 are open.Switches S2, S5, S8, S11, S14, S17, S20 and S23 are open and switchesS4, S7, S10, S13, S16, S19, S22 and S25 are closed. Switch 26 is nowopened and switch 28 is now closed, connecting batteries V1, V2, V3, V4,V5, V6, V7, V8 and V9 in series with the SSC output.

The SSC 650 now switches back to CHARGE mode and charges the PFN from9200 to 10200 volts by the series voltage addition of SSC Vout and V1,V2, V3, V4, V5, V6, V7, V8, V9 (9 kV). Vout varies over a range from0-1200 volts. At PFN full charge voltage of 10200 Volts, the SSC currentdrops to zero and then acts as a voltage regulator maintaining thecharge in the PFN at the proper voltage.

Step 11—De-Erecting:

Just prior to firing the PFN capacitor bank 680, the SSC 650 is shut offand all the switches are opened. In the event of a short, the HVcontactor S1 is opened and the SSC 650 is shut off and all of theswitches are opened.

FIG. 7 depicts an alternative embodiment of the invention 700. In thisembodiment, the system consists of several ERB arms 701, 702, 703, and704, configured in a “star” configuration 712. The redundancy of thisconfiguration has several advantages including fault tolerance. Switchsteering matrices are connected to both the inner 713 and outer portionsof the star configurations. The ERB arms are connected at one end to theparallel low voltage or baseline voltage 705 and at the other end to thevariable high voltage load 706. Each of the two ends of an ERB arm (e.g.701) has a bi-directional power output connection. The energy from thebase side connection 713 of each arm (e.g. 701) is fed in parallel tothe center switch matrix to provide traction power for the main systemload. The outer switch matrix consists of positive diode switch matrix710, negative diode matrix 711 and switch 708 and switch 714 locatedbelow the capacitor below storage capacitor 707.

Diode switches 710 and 711 are voltage controlled switches that areturned on when the differential voltage between the arm output and thecapacitor terminal forward bias the voltage across the diodes. The diodedisconnect when the voltage differential between the capacitor and theindividual arm output results in reverse biasing if one arm or both armsoutput voltage are below the capacitor voltage the one or both arms aredisconnected by the diodes.

Normal operation is when the modules are de-erected and disconnectedcausing diode switch matrices 710,711 to be back biased resulting inturning off the switches, then switch 708 and the other switch by baseare then turned on to connect the energy stored in capacitor 707 to betransferred to the load.

The energy stored in each arm can also be directed out the opposite end710 to be directed through the VHV connection into the outer switchmatrix 708. Additionally the energy flow is in discrete energy packetsthat are time multiplexed on the VHV connection side while maintaining acontinuous connection and energy flow through the base or parallelconnection side 713. Additionally, energy from one ERB arm (e.g. 701)can be transferred to another ERB arm (e.g. 702). A simple switchingalgorithm and a three-switch one diode configuration can be used toguarantee no catastrophic battery or file failure due to mistiming ofthe high-speed switching. This is accomplished by switching off oropening all of the positive or negative rail switches and then usingjust one series switch connection and one required steering diode permodule to erect and de-erect the batteries or capacitors that are inseries.

Alternatively, the base switch matrix can be set to “ON” (i.e. theswitch closed) at all times by replacing it with hard wired parallelconnections of the base voltage terminals. The invention allows simplescaling by the simple addition of more modules without any rewiring.Sophisticated ERB systems with complete redundancy of the ERB star andmultiple star configurations are easily configured by switched in andcross connected at the base and or at the VHV level matrix levels.

In an alternative embodiment, for the purposes of redundancy andreliability, the VHV outputs are steered in parallel operation through asimple VHV diode steering array. This allows complete or partial failureof one or more ERB arms 701, 702, 703, or 704 while maintaining functionof the entire system. For instance the system 700 depicted in FIG. 7 cansuffer a complete failure of one plus (e.g. 701) and one minus outputERB arm (e.g. 702) and still meet most of the requirements of the VHVload. When used for powering an electric or gas-electric hybrid, thesystem can suffer the loss of three ERB arms before loosing traction ormoving capability.

As can be seen from FIG. 8, each of the ERB arms 801 is comprised ofseveral ERB modules 802. Each ERB module 802 contains an energy storagedevice 803, such as a battery or capacitor, and piece of the distributedmodular bus structure and steering array. It would be understood by oneskilled in the art that any of the modular diagrams disclosed in FIGS.1-6 could be used to construct an ERB arm.

FIG. 9 illustrates another embodiment of the invention. Each ERB arm 910consists of a scalable number of ERB modules 920. In such an embodimenteach module 920 contains an energy source, part of the modulardistributed series and parallel switch matrix and bus bar system, andthe fusing and protection as well as the control systems. While thepreferred embodiment has two input power ports 960 and two output powerports 950, any number of power ports could be used. The ERB arms arescaled by connecting an output port 950 of a first module 920 to aninput port 960 of a second module 930 to create a module string. Thiscan be done for a plurality of ERB modules with the final module 970 inthe string connecting to the VHV steering array 940. Very high voltagescan be achieved in this fashion. Because this application of the ERBmodules is scalable, the number of modules per ERB arm is applicationdriven and, in a multiple arm ERM “star” configuration system, each armmay have a different number of modules and have a different polarizationof output voltage to satisfy a wide variety of load requirements.

In examples shown in FIGS. 7 and 8 and described above, 2 identical setsof one positive and one negative stackable module arms were chosen withthe positive 5000 volt arms and HV outputs shown on the left and thenegative 5000 volt arms and HV outputs shown on the right. One half ofhigh voltage steer able diode switch matrix was added to each side soany number of arms can be added in parallel.

The purpose of splitting the module chain or arms in half was to reducethe number of modules per arm connected to a common center parallel basecore buss thus reducing the battery system ESR (Equivalent Seriesresistance) by a factor of 4 in the parallel mode and increasereliability by having 4 parallel arms vs. 2 arms. Also by splitting intopositive and negative arms the differential voltage is double thevoltage to reference to ground simplifying insulation systems

Not shown are that multiple high voltage switch matrixes and loads canbe shared among multiple stars. The Low Voltage parallel arm end (basein FIG. 7) are connected to a common star low voltage buss or batterysystem and outer end or HV end of each arm can be connected to a single,or multiple outer switch high voltage switch matrixes,

An 8 arm star (star-1) can be implemented by adding four more arms tothe H configuration with 8 arms of stackable modules with 4 armsconnected to HV matrix—one connected to pulsed laser system, arms 5-6connected to HV Switch matrix—2 and Pulsed Microwave system, arms 7-8connected HV traction system.

Thus, additional stars can add their arms outputs and be cross-connectedat both the inner outer hubs or arm ends to the Star-1 for redundancy ormore power.

Thus, a number of preferred embodiments have been fully described abovewith reference to the drawing Figs. Although the invention has beendescribed based upon these preferred embodiments, it would be apparentto those of skill in the art that certain modifications, variations, andalternative constructions could be made to the described embodimentswithin the spirit and scope of the invention. Further, as should beapparent to one skilled in the art after reviewing this patent document,the modular battery system of the present invention could be useful ininnumerable other applications not listed here.

1. An electronically reconfigurable battery, comprising: a firstplurality of battery modules configured in a star configuration; aplurality of switches interconnecting said plurality of battery modulessuch that a selectable number of said plurality of battery modules maybe connected either in a series configuration or in a parallelconfiguration, as a result of placing selected switches of saidplurality of switches in open states or closed states; and an outputswitch for connecting a first output terminal of said battery to a firstload.
 2. An electronically reconfigurable battery as recited in claim 1,wherein each of said plurality of battery modules is coupled with atleast three of said plurality of switches as follows: a first switchwhich connects said each battery module in series with an adjacentbattery module when closed, and second and third switches which connectsaid each battery module in parallel with an adjacent battery modulewhen closed, wherein when said first switch is closed, said second andthird switches are open, and when said first switch is open, said secondand third switches are closed.
 3. An electronically reconfigurablebattery as recited in claim 1, further comprising: a second plurality ofbattery modules, each of said second plurality of battery modules beingconnected in parallel with each other, said first plurality of batterymodules being selectively connected to said second plurality of batterymodules through at least two of said plurality of switches.
 4. Anelectronically reconfigurable battery as set forth in claim 3, furthercomprising a second output terminal for connecting said second pluralityof battery modules to a second load.
 5. An electronically reconfigurablebattery as set forth in claim 4, wherein said second load comprises amotor for propelling a vehicle or vessel.
 6. An electronicallyreconfigurable battery as set forth in claim 5, wherein said first loadcomprises an electromagnetic armor system.
 7. An electronicallyreconfigurable battery as set forth in claim 1, wherein said pluralityof switches comprises a plurality of integrated gate bipolar transistor(IGBT) switches.
 8. An electronically reconfigurable battery as setforth in claim 1, wherein said plurality of switches comprises aplurality of metal oxide field effect transistor (MOSFET) switches. 9.An electronically reconfigurable battery as set forth in claim 7, wherein said plurality of IGBT switches comprise opto-isolated switches. 10.An electronically reconfigurable battery as set forth in claim 8,wherein said plurality of MOSFET switches comprise opto-isolatedswitches.
 11. A hybrid electric vehicle, comprising: a primary mover forproviding a primary source of propulsion energy to a vehicle load; anelectronically reconfigurable battery for providing a secondary sourceof propulsion energy to said vehicle load, and for providing a source ofenergy for a short-term and/or pulsed load provided on said vehicle,said electronically reconfigurable battery comprising a first pluralityof battery modules configured in a star configuration; a plurality ofswitches selectively interconnecting said plurality of battery modules,wherein a number of said plurality of battery modules may be selectivelyconnected either in a series configuration or in a parallelconfiguration, as a result of placing selected switches of saidplurality of switches in open states or closed states; an output switchconnecting a first output terminal of said battery to said short-termand/or pulsed load; and a second output terminal of said battery beingconnected to said vehicle load.
 12. A hybrid electric vehicle as setforth in claim 11, wherein each of said plurality of battery modules iscoupled with at least three of said plurality of switches as follows: afirst switch which connects said each battery module in series with anadjacent battery module when closed, and second and third switches whichconnect said each battery module in parallel with an adjacent batterymodule when closed, wherein when said first switch is closed, saidsecond and third switches are open, and when said first switch is open,said second and third switches are closed.
 13. A hybrid electric vehicleas recited in claim 11, further comprising a second plurality of batterymodules, each of said second plurality of battery modules beingconnected in parallel, said first plurality of battery modules beingselectively connected to said second plurality of battery modulesthrough at least two of said plurality of switches.
 14. A hybridelectric vehicle as recited in claim 11, wherein said vehicle loadcomprises a motor for propelling said vehicle.
 15. A hybrid electricvehicle as recited in claim 11, wherein said short-term and/or pulsedload comprises an electromagnetic armor system for said vehicle.
 16. Ahybrid electric vehicle as recited in claim 11, wherein said pluralityof switches comprises a plurality of IGBT switches.
 17. A hybridelectric vehicle as recited in claim 11, wherein said plurality ofswitches comprises a plurality of MOSFET switches.
 18. A hybrid electricvehicle as recited in claim 16, wherein said plurality of IGBT switchesare opto-isolated switches.
 19. A hybrid electric vehicle as recited inclaim 17, wherein said plurality of MOSFET switches are opto-isolatedswitches.
 20. An electronically reconfigurable battery as recited inclaim 1, wherein said reconfigurable battery can be reconfigured tomatch a hybrid vehicle with a variable DC main bus voltage used for afirst level of reliability and to shorter life higher power mode.
 21. Anelectronically reconfigurable battery as described in claim 1, whereinDC current is limited by selection of electrochemical dischargecharacteristics of the selected battery technology.
 22. Anelectronically reconfigurable battery as described in claim 1, furthercomprising a series current limiting device inserted in circuit with thefully erected battery so as to limit DC current.
 23. An electronicallyreconfigurable battery as described in claim 1, further comprising aseries current limiting device inserted in circuit with the partially orsequential erected battery so as to limit DC current.
 24. Anelectronically reconfigurable battery as described in claim 23, whereinsaid charge current limiting device comprises a single stage converter(SSC) whose output voltage is limited to approximately the batterymodule voltage level.
 25. An electronically reconfigurable battery asdescribed in claim 24, wherein a bypass switch is used to connect theinput to the output of the SSC circuit to directly connect the dynamicstore portion of the battery with the static portion of the battery. 26.An electronically reconfigurable battery as described in claim 22,wherein said current limiting device comprises a resistive or inductivecomponent in a resistance-capacitance (RC) or inductance-capacitance(LC) current limiting circuit.
 27. An electronically reconfigurablebattery as described in claim 23, where the current limiting devicecomprises resistive or inductive component in a RC or LC currentlimiting circuit.
 28. An electronically reconfigurable battery asdescribed in claim 24, wherein the SSC comprising an electronic DC-DCconverter whose input circuit is connected to the static portion of thebattery and whose output is connected to the first stage of the dynamicsection of the battery.
 29. An electronically reconfigurable battery asdescribed in claim 24, wherein the SSC comprising an electronic DC-DCconverter whose input circuit is connected to a suitable DC source otherthan the static portion of the battery and the output is connected tothe first stage of the dynamic section of the battery.
 30. Anelectronically reconfigurable battery as described in claim 24, whereinthe SSC comprises an electronic converter whose circuit topology ischosen from the group consisting of Buck, Boost, Buck/Boost, step-up,step-down, resonant, isolated, non-isolated, cyclo-converter, and matrixconverter.
 31. An electronically reconfigurable battery as described inclaim 24, wherein the SSC comprises an electronic AC-DC converter whoseinput circuit is connected to a suitable AC source and whose output isconnected to the first stage of the dynamic section of the battery. 32.An electronically reconfigurable battery as described in claim 1,wherein said battery is adapted for use in high to extreme peak toaverage power output pulsed power applications and platforms fornon-vehicular applications.
 33. An electronically reconfigurable batteryas described in claim 1, wherein each arm of the configuration comprisesa plurality of ERB modules which can be strung together based on theneeds of the particular application.
 34. A reconfigurable battery systemcomprising: a plurality of battery arms, each battery arm comprising aplurality of battery modules which are electronically reconfigurable toselectively operate in parallel or series; a center switch matrixcoupled with a first output terminal and each of said battery arms, andconfigured to selectively connect one or more of said battery arms withsaid first output terminal; an outer switch matrix coupled with a secondoutput terminal and each of said battery arms, and configured toselectively connect one or more of said battery arms with said secondoutput terminal.
 35. The reconfigurable battery system as recited inclaim 34, wherein said center switch matrix couples the first outputterminal with each said battery arm on a first battery arm side thereof,and said outer switch matrix couples the second output terminal witheach battery arm on a second battery arm side thereof.
 36. Thereconfigurable battery system of claim 34, wherein the plurality ofbatter arms comprises a first battery arm, a second battery arm, a thirdbattery arm and a fourth battery arm.
 37. The reconfigurable batterysystem of claim 34 wherein each battery arm comprises a scalable numberof battery modules.